STC SA608GL
FAA DRS lists SA608GL as Current · Reissued, held by Shadin Avionics, for Piper Aircraft PA-23-250 (Navy UO-1) and Piper Aircraft PA-E23-250. Recorded change: Installation of a Shadin Co. 910502 or 910504 fuel flow indicating system. Snapshot dated June 30, 2026.
Recorded modification
What the FAA record covers
SA608GL identifies the approval, recorded holder, named aircraft, and modification scope. It does not confirm kit availability, serial-number effectivity, data rights, price, or installation authority.
Applicability
Aircraft named in FAA DRS
Named aircraft: Piper Aircraft PA-23-250 (Navy UO-1) and Piper Aircraft PA-E23-250. Confirm the approved model list, serial effectivity, configuration, and certificate revision.
Related fuel systems STCs
Installation of Floscan -201b or -203b fuel flow transducers.
FAA holder: RAM Aircraft Limited Partnership
Installation of an Isolated Fuel Quantity Transmitter in Continental Model 737-300 airplanes using Simmonds Precision Document No. V-1477, 'Installation Instructions for the Isolated Fuel Quantity Transmitter System applicable to 737-300, 737-500, Classic Series Aircraft' dtd 11/16/01 or later FAA-approved revision.
FAA holder: Simmonds Precision Products Inc
FAA record reference
- STC number
- SA608GL
- Product
- Aircraft · Small Multi-Engine
- Country
- United States
- Application date
- November 14, 1981
- Revision date
- June 8, 2006
- CFR references
- Part 3, Part 21